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  • session 4

    Title

    Guidance, Navigation & Control (2)

    Description

    The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft and rockets, including formation flying, rendezvous and docking.

    Date

    2017-09-27

    Time

    09:45

    Room

    Hall A

    IPC members
    • Co-Chair: Dr. Anton de Ruiter, Ryerson University, Canada;

    • Co-Chair: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;

    • Rapporteur: Prof. Igor V. Belokonov, Samara National Research University (Samara University), Russian Federation;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Stabilization of Underactuated Spacecraft with Two CMGs using Model Predictive Control

    15

    withdrawn

    Dr. Haichao Gui

    Ryerson University

    Canada

    2

    Comparison of EKF and UKF for Robotic Missions to Mars

    15

    confirmed

    Mr. Jeffrey Stuart

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    3

    Parallel Spacecraft Solar and Thermal Radiation Pressure Modeling Using Graphic Processing Unit

    15

    confirmed

    Mr. Patrick Kenneally

    The University of Colorado

    United States

    4

    Ascent Flight Control of Launch Vehicle Using Angle of Attack Estimator

    15

    withdrawn

    Mr. Ario Birmiawan Widyoutomo

    The Graduate Universty for Advanced Studies (SOKENDAI)

    Japan

    5

    Docking of a space tug with upper stage debris object using deployable flexible beam

    15

    confirmed

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    6

    a paper and pencil method of evaluating trajectories of space launchers

    15

    confirmed

    Prof. Paolo Teofilatto

    Sapienza - University of Rome

    Italy

    7

    distributed coordinated finite-time attitude tracking control for multiple networked spacecraft systems with unknown deadzone

    15

    confirmed

    Dr. ZHIYONG SHE

    Beijing Aerospace Technology Institute

    China

    8

    New Implicit Neighboring Optimal Guidance and Attitude Control for Three-dimensional Lunar Ascent

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza - University of Rome

    Italy

    9

    Tether length control in tether-assisted deorbiting mission from an elliptical orbit

    15

    confirmed

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    10

    magneto-coulombic fault tolerant sliding mode attitude control of earth pointing satellites

    15

    confirmed

    Mr. Himanshu Prabhat

    IIT Kharagpur

    India

    11

    Orientation Optimisation of a Four Reaction Wheel Satellite Control System for Fault Tolerance

    15

    confirmed

    Dr. Zebb Prime

    Australia

    12

    Launch Vehicle Adaptive Flight Control with Incremental Model Based Heuristic Dynamic Programming

    15

    confirmed

    Ms. Ye Zhou

    Delft University of Technology (TU Delft)

    The Netherlands